Swash plate system for helicopter rotor
A device for controlling a collective pitch and a cyclic pitch of rotor blades of a rotoreraft of a direct turbine driven type and contra-rotating coaxial rotor type (DTDR) includes: a lower rotor and an upper rotor that are mounted concentrically on a shared rotor shaft; a first plate, that is not rotatable, fastened to a structure of the rotorcraft and connected to an actuator that communicates collective pitch and cyclic pitch controls to it, the first plate being mounted so as to be movable in translation along the shared rotor shaft and to oscillate relative to the shared rotor shaft, via a lower ball joint mechanism; and a second plate, that is rotatable, housed on the lower ball joint mechanism so as to be always parallel to the first plate, the second plate being driven in rotation by a member connecting it to the lower rotor.
1. A device for controlling a collective pitch and a cyclic pitch of rotor blades of a rotorcraft of a direct turbine driven type and contra-rotating coaxial rotor type (DTDR), comprising:
a lower rotor and an upper rotor that are mounted concentrically on a shared rotor shaft;
a first plate, that is not rotatable, fastened to a structure of the rotorcraft and connected to an actuator configured to communicate collective pitch and cyclic pitch controls to it, the first plate being mounted so as to be movable in translation along the shared rotor shaft and to oscillate relative to the shared rotor shaft, via a lower ball joint mechanism;
a second plate, that is rotatable, housed on the lower ball joint mechanism so as to be always parallel to the first plate, the second plate being driven in rotation by a member connecting it to the lower rotor and being connected to a pitch control lever of each blade of the lower rotor by a lower connecting rod;
a third plate and a fourth plate, both rotatable being driven in rotation by a member connecting them to the lower rotor or to the upper rotor and housed on an upper ball joint mechanism so as to be always parallel to one another, the fourth plate being connected to a pitch control lever of each blade of the upper rotor by an upper connecting rod;
means for ensuring that the third plate is always parallel to the second plate so that the third plate receives a same translation and a same tilt as the second plate by the respective collective pitch and cyclic pitch controls,
wherein a length of the pitch control levers of the blades of the lower rotor is smaller than a length of the pitch control levers of the blades of the upper rotor, so that a different collective pitch variation on the blades of the upper rotor and on the blades of the lower rotor is ensured.
2. The device according to claim 1 , wherein the means for ensuring that the third plate is always parallel to the second plate comprises a plurality of connecting rods equal in length between the second plate and the third plate, and which are parallel to the shared rotor shaft.
3. The device according to claim 2 , wherein a number of the connecting rods is at least equal to three.
4. The device according to claim 1 , wherein, alternatively, the third plate is connected to the pitch control lever of each blade of the lower rotor by a lower connecting rod.
5. The device according to claim 1 , wherein, for a given travel imposed by the collective pitch control, a ratio between a pitch control lever arm of the blades of the upper rotor and a pitch control lever arm of the blades of the lower rotor is greater than one, which corresponds to a maximum angular variation of the pitch of the lower rotor greater than a maximum angular variation of the pitch of the upper rotor.